Lightweight titanium aluminide valves and methods for the manufacture thereof

ABSTRACT

Embodiments of a lightweight, high temperature airborne valve are provided. In one embodiment, the airborne vale includes a valve element and a flowbody. The flowbody is formed at least partially from a titanium aluminide alloy and has a flow passage therethrough in which the valve element is movably mounted. Embodiments of a method for producing such a lightweight, high temperature airborne valve are also provided. In one embodiment, the method includes the steps of forming a lightweight flowbody at least partially from a titanium aluminide alloy, hot isostatically pressing the lightweight flowbody, and machining the lightweight flowbody to desired dimensions.

CROSS-REFERENCE TO RELATED APPLICATION

This application is a divisional of co-pending U.S. application Ser. No.12/549,098, filed Aug. 27, 2009.

TECHNICAL FIELD

The present invention relates generally to valves and, moreparticularly, to embodiments of lightweight valves well suited for usein high temperature airborne applications, such as deployment aboard anaircraft.

BACKGROUND

Airborne valves are commonly deployed aboard aircraft to regulate fluidflow. An airborne valve, and specifically the material from which theflowbody of the airborne valve is cast, ideally has relatively lowdensity, is highly durable, and is highly ductile. When intended tooperate in lower temperature environments, airborne valve flowbodies arecommonly cast from aluminum and aluminum-based alloys, which generallysatisfy the foregoing criteria. However, when the airborne valve is tobe utilized within higher temperature environments (e.g., approachingand possibly exceeding approximately 1,200° Fahrenheit), such as whenthe airborne valve is used to regulate compressor or combustive gas flowfrom a gas turbine engine, aluminum and aluminum-based alloys aretypically unsuitable as flowbody materials due to operationaltemperature limitations. For this reason, it is conventional practice inaerospace industry to cast high temperature valve flowbodies fromhigh-strength, refractory metal alloys, such as 17-4PH stainless steelor Inconel 718®. Although durable and relatively ductile, suchrefractory metal alloys have relatively high densities (e.g., thedensities of 17-4PH stainless steel and Inconel 718® are approximately7.74 grams per cubic centimeter (g/cm³) and 8.22 g/cm³, respectively).Airborne valve flowbodies cast from such high temperature materials areconsequently undesirably heavy for utilization in airborne applications.

Titanium aluminide alloys have relatively low densities and have beenutilized to fabricate certain dynamic components deployed within gasturbine engine, such as air turbine blades. However, titanium aluminidealloys have long been considered excessively brittle for use in thefabrication of high temperature airborne flowbodies, which serve aspressure vessels that conduct highly pressured fluids during operation(e.g., pressured bleed air having pressures exceeding several hundredpounds per square inch (psi) and commonly approaching 600 psi). Titaniumaluminide alloys have also been utilized to produce certain non-pressurecontaining valve components (e.g., poppet-type valve elements) for otherground-based pneumatic systems, such as for automotive internalcombustion engines. Titanium aluminide alloys have not, however, beenutilized to produce static, pressure-containing valve flowbodies in anycontext of which the present inventors are aware. Furthermore, in theterrestrial applications set-forth above, the operational requirements,the valve types, and the valve designs are markedly disparate from thehigh temperature, high pressure airborne valve flowbodies utilized inthe aerospace industry.

There thus exists an ongoing need to provide embodiments of a hightemperature airborne valve having a reduced weight as compared toconventional airborne valves produced utilizing high density material,such as 17-4PH stainless steel and Inconel 718®. In accordance withembodiments of the present invention, and as described in the subsequentsections of this document, this ongoing need is satisfied by providingairborne valves including lightweight flowbodies formed, at least inpart, from titanium aluminide. It would also be desirable to provide oneor more methods for manufacturing such lightweight, high temperatureairborne valves. Other desirable features and characteristics of thepresent invention will become apparent from the subsequent DetailedDescription and the appended claims, taken in conjunction with theaccompanying drawings and this Background.

BRIEF SUMMARY

Embodiments of a lightweight, high temperature airborne valve areprovided. In one embodiment, the airborne valve includes a flowbody anda valve element. The flowbody is formed at least partially from atitanium aluminide alloy and has a flow passage therethrough in whichthe valve element is movably mounted.

Embodiments of a pneumatic avionic system for deployment aboard anaircraft are further provided. In one embodiment, the pneumatic avionicsystem includes an aircraft duct and a lightweight, high temperatureairborne valve fluidly coupled to the aircraft duct. The lightweight,high temperature airborne valve includes a flowbody having a flowpassage therethrough, and a valve element movably mounted within theflow passage for modulating fluid flow therethrough. The flowbody isformed at least partially from a titanium aluminide alloy.

Embodiments of a method for producing such a lightweight, hightemperature airborne valve are still further provided. In oneembodiment, the method includes the steps of forming a lightweightflowbody at least partially from a titanium aluminide alloy, hotisostatically pressing the lightweight flowbody, and machining thelightweight flowbody to desired dimensions.

BRIEF DESCRIPTION OF THE DRAWINGS

At least one example of the present invention will hereinafter bedescribed in conjunction with the following figures, wherein likenumerals denote like elements, and:

FIG. 1 is an isometric view of a lightweight, high temperature airbornevalve including a flowbody formed at least partially from titaniumaluminide in accordance with a first exemplary embodiment;

FIG. 2 is an exemplary manufacturing process suitable for producing alightweight, high temperature airborne valve having a flowbody castsubstantially entirely from titanium aluminide in accordance with afurther exemplary embodiment; and

FIGS. 3-8 are generalized cross-sectional views of an exemplarylightweight, high temperature airborne valve at various stages ofmanufacture and produced in accordance with the exemplary manufacturingprocess illustrated in FIG. 2.

DETAILED DESCRIPTION

The following Detailed Description is merely exemplary in nature and isnot intended to limit the invention or the application and uses of theinvention. Furthermore, there is no intention to be bound by any theorypresented in the preceding Background or the following DetailedDescription.

FIG. 1 is an isometric view of a lightweight, high temperature airbornevalve 20 suitable for deployment onboard an aircraft in accordance withan exemplary embodiment. Airborne valve 20 includes a flowbody 22 havinga flow passage or axial bore 24 therethrough. By way of non-limitingexample, flowbody 22 is illustrated in FIG. 1 as having a generallycylindrical shape and including the following features: (i) first andsecond plate structures 26 to which a valve actuator (not shown) orother component may be mounted, (ii) a tubular structure 28 extendingbetween plate structures 26 and through which a drive shaft (not shown)may extend, (iii) a plurality of bosses 30, and (iv) first and secondradial flanges 32 and 34, which are provided around first and secondopposing ends of flowbody 22, respectively. When high temperatureairborne valve 20 is fully assembled, a valve element (hidden from viewin FIG. 1) is mounted within axial bore 24. In the illustrated example,specifically, a butterfly plate may be disposed within axial bore 24 andmounted on a rotatable drive shaft (not shown), which is, in turn,mechanically coupled to valve actuator (also not shown). This examplenotwithstanding, the valve element may assume any form suitable formodulating fluid flow through the flow passage of airborne valve 20. Forexample, in embodiments wherein high temperature airborne valve 20assumes the form of a right-angle poppet valve or an inline poppetvalve, the valve element disposed within axial bore 24 may be a poppet.

In accordance with the teachings of the present invention, flowbody 22is formed at least partially from a titanium aluminide (TiAl) alloy;and, in a preferred group of embodiments, flowbody 22 is castsubstantially entirely from a titanium aluminide alloy. Still morepreferably, flowbody 22 is cast from a titanium aluminide alloy that isnear-stoichiometric (i.e., has a titanium to aluminum ratio ofapproximately 1:1 on the atomic scale) and/or that has a density in therange of approximately 3.5 g/cm³ to approximately 5.0 g/cm³. Notably,titanium aluminide alloys have relatively low densities as compared tothe high-strength, refractory metal alloys, such as 17-4PH stainlesssteel and Inconel 718®, conventionally utilized to produce valveflowbodies in the aerospace industry. As a result, flowbody 22 weighssignificantly less than a similar flowbody formed from a conventionalrefractory metal alloy. At the same time, TiAl flowbody 22 is operablein high temperature and high pressure environments; e.g., operationalenvironments characterized by temperatures approaching or exceeding1200° Fahrenheit and pressures approaching or exceeding several hundredpsi. TiAl flowbody 22, and more generally airborne valve 20, isconsequently well suited for deployment aboard an aircraft as a meansfor regulating the flow of a heated and highly pressurized fluid, suchas combustive gas flow bled from the combustor of a gas turbine engine.

It will be appreciated that the terms “titanium aluminide alloy” and“TiAl alloy” are utilized to denote an alloy containing titanium andaluminum as the primary constituents. A given titanium aluminide alloycan, and typically will, include lesser amounts of one or moreadditional metallic or non-metallic constituents. A non-exhaustive listof additional components that may be contained within a particulartitanium aluminide alloy includes manganese, boron, niobium, molybdenum,titanium diboride, and the like. Such additive components may be addedin powder form to a master alloy during processing to optimize themetallurgical properties of the resulting titanium aluminide alloy.

As previously noted, titanium aluminide alloys have been utilized in theproduction of dynamic components deployed within gas turbine engine,such as air turbine blades. In addition, titanium aluminide alloys havebeen utilized to fabricate valve elements in automotive internalcombustion engines. However, titanium aluminide alloys have notconventionally been utilized to produce a flowbody or pressure vesselincluded within an airborne valve. Indeed, it has long been believedwithin the aeronautical field that titanium aluminide alloys areunsuitable for use in the production of pressure vessels due to therelatively low ductility, and therefore the relative brittleness, oftitanium aluminides. However, contrary to this long held belief, thepresent inventors have discovered that, in principle, certain titaniumaluminide alloys can be utilized to produce airborne valve flowbodiescapable of operating at elevated temperatures and pressurescharacteristic of avionic applications. Furthermore, the presentinventors have discovered that by producing airborne valve flowbodiesfrom titanium aluminide, in substantial part or in entirety, asubstantial weight savings can be realized as compared to airborne valveflowbodies formed from conventional high temperature materials, such as17-4PH stainless steel and Inconel 718®.

FIG. 2 is a flowchart illustrating an exemplary method 40 suitable forproducing a lightweight, high temperature airborne valve including aTiAl flowbody. FIGS. 3-8 illustrate in cross-section a generalizedairborne valve 42 at various stages of manufacture and produced inaccordance with exemplary method 40 (FIG. 2). In this particularexample, airborne valve 42 assumes the form of a cylindrically-shapedbutterfly valve; however, it is emphasized that method 40 can beutilized to produce any suitable type of airborne valve, includingvarious types of poppet valves. To commence exemplary method 40 (STEP44), a mold is provided that defines the general shape and approximatedimensions of airborne valve 42. For example, and with reference to FIG.3, a lost wax mold 46 having a skin formed from ceramic or other hightemperature material can be produced during STEP 44 in the well-knownmanner (e.g., by producing a model from wax or other sacrificialmaterial having a relatively low melting point, forming a ceramic moldover the model, and then heating the mold/model to a temperaturesufficient to melt the model and thus produce a cavity within the mold).Airborne valve 42 is preferably cast slightly oversized and subsequentlymachined to desired dimensions as described more fully below.

Next, at STEP 48, the particular titanium aluminide alloy that willultimately be utilized to form the flowbody of airborne valve 42 isselected. As indicated in FIG. 2, the particular titanium aluminidealloy selected during STEP 48 is typically chosen based, at least inpart, upon the environmental and operational requirements of airbornevalve 42. As a general example, a group of candidate titanium aluminidealloys can first be identified based upon minimal strength requirements,and then the most ductile alloy within the group of candidate titaniumaluminide alloys may be selected for use. In a preferred group ofembodiments, a titanium aluminide alloy that is near-stoichiometric(i.e., that has an atomic ratio of Ti to Al of approximately 1:1) and/orthat has a density between approximately 3.5 g/cm³ to approximately 5.0g/cm³ is chosen during STEP 48.

After selection of a desired titanium aluminide alloy (STEP 48), thetitanium aluminide is heated and melted in an appropriate enclosuresubstantially devoid of oxidants, poured into mold 46 in molten form,and then allowed to solidify to produce a lightweight TiAl flowbody 50(STEP 52). TiAl flowbody 50 is then removed, partially or entirely, frommold 46. In the exemplary embodiment illustrated in FIG. 4, TiAlflowbody 50 is formed to include a flow passage (i.e., an axial bore) 54therethrough, a first radial mounting flange 56 integrally formed arounda first end portion of TiAl flowbody 50, and a second radial mountingflange 58 integrally formed around a second opposing end portion of TiAlflowbody 50. As indicated in FIG. 4 by centerline 60, TiAl flowbody 50,first radial flange 56, and second radial flange 58 each have agenerally annular three-dimensional form; however, it is againemphasized that the particular geometries and structural features ofTiAl flowbody 50 and, more generally, of airborne valve 42 willinevitably vary amongst different embodiments.

Continuing with exemplary method 40 (FIG. 2), TiAl flowbody 50 nextundergoes a hot isostatic pressing or HIP process (STEP 62) in anappropriate environment. As indicated in FIG. 5 by heat lines 64, TiAlflowbody 50 is subjected to elevated pressures and temperatures for apredetermined time period during the HIP process to consolidate thetitanium aluminide alloy microstructure. In certain embodiments, acharacterization process may then be performed during which TiAlflowbody 50 is examined for structural defects utilizing X-rayradiography or another inspection technique before advancing to STEP 66of exemplary method 40 (FIG. 2). Subsequent to the HIP process, one ormore high temperature treatments (HTTs) are conveniently, although notnecessarily, performed in an appropriate environment (STEP 66). As willbe readily appreciated, during each HTT, TiAl flowbody 50 is subjectedto an elevated temperature for a predetermined time period to refine andfurther reduce residual stresses within the TiAl alloy microstructure.In certain embodiments, a characterization process may then be performedduring which TiAl flowbody 50 is examined for structural defectsutilizing X-ray radiography or another inspection technique beforeadvancing to STEP 68 of exemplary method 40 (FIG. 2).

During STEP 68 of exemplary method 40 (FIG. 2), one or more surfaces orstructural features of TiAl flowbody 50 are machined to desireddimensions. For example, as indicated in FIG. 6 by arrows 70, radialmounting flanges 56 and 58 may be machined to fine tune the dimensionsthereof. Additionally or alternatively, thickness may be removed fromthe inner surfaces of TiAl flowbody 50 to bring the diameter of axialbore 54 to within a relatively close tolerance of a target dimension(indicated in FIG. 6 by arrows 72). Various other features may also beformed on, through, or within TiAl flowbody 50 during STEP 68 (e.g.,holes may be drilled through mounting features provided on TiAl flowbody50 to receive bolts or other mechanical fasteners). To this end, anysuitable machining technique or combination of techniques can beemployed during STEP 68 including, but not limited to, mechanicalmachining (e.g., grinding, mechanical turning, etc.), chemical milling,laser ablation, and the like.

To conclude exemplary method 40 (FIG. 2), various additional fabricationsteps are performed to complete fabrication of airborne valve 42 (STEP70). For example, as illustrated generically in FIG. 7, a valve element74 (e.g., a butterfly disc) is mounted within axial bore 54 providedthrough airborne valve 42. Disc element 74 may include a wiper seal thatsealingly engages an inner surface of the axial bore. A wear-resistantcoating 76 may optionally be applied over the inner surface of TiAlflowbody 50 defining axial bore 54 or, at minimum, the area of axialbore 54 sealingly engaged by valve element 74 through its range ofmotion. Wear-resistant coating 76 is enlarged in FIG. 7 for clarity. Inembodiments wherein valve element 74 assumes the form of a poppet orother translating member, a wear-resistance coating may also benecessary. Other coatings may also be applied over one or more surfacesof airborne valve 42 during STEP 70 including, for example, anoxidation-resistant coating. For example, as indicated in FIG. 7 at 77,an oxidation-resistant coating can be applied to all surfaces or toselected surfaces of flowbody 50 (e.g., to the surfaces exposed to hotgas flow during operation of valve 42), as appropriate. As should bereadily appreciated, oxidation-resistant coating 77 is only partiallyshown and enlarged in FIG. 7 for clarity. Finally, a characterizationprocess may be performed utilizing X-ray radiography or anotherinspection technique to ensure that airborne valve 42 is substantiallyfree of structural defects.

After fabrication, airborne valve 42 can be installed within a pneumaticavionic system deployed aboard an aircraft. For example, with referenceto FIG. 8, airborne valve 42 is installed within pneumatic avionicsystem including an aircraft duct 78. More specifically, radial mountingflange 56 of TiAl flowbody 50 is clamped (e.g., utilizing, for example,a V-band clamp 80) to a corresponding radial flange 82 provided aroundduct 78 such that the radial face of radial mounting flange 56 abuts andis held against the radial face of radial flange 82. An alternate flangedesign and sealing method may include a groove formed in at least one ofthe two mating flanges and an appropriate gasket or O-ring, such as ametallic gasket, inserted into the groove to provide required sealingover the operating temperature and pressure ranges of the valveassembly. During operation of the pneumatic avionic system, TiAlflowbody 50 of airborne valve 42 conducts a heated, pressurized fluid,such as compressor or combustive gas flow, either to or from aircraftduct 78. As previously stated, TiAl flowbody 50 is especiallywell-suited for this purpose due to its reduced weight and ability tomaintain its structural integrity at relatively high operationaltemperatures.

Exemplary Embodiments of Titanium Aluminide Airborne Valve FlowbodiesReduced to Practice

By way of illustration and not of limitation, the following tableprovides the composition of two titanium aluminide alloys utilized toproduce airborne valve flowbodies in actual practice. Duringmanufacture, the titanium aluminide alloys were each liquefied andpoured into one or more ceramic molds within an appropriate enclosuresubstantially devoid of oxidants. Then, after solidification of thecorresponding flowbodies, the latter were removed from the ceramicmolds. The resulting valve flowbodies were then subjected to additionalprocessing steps (e.g., hot isostatic pressing) and subsequentlyweighed. Two airborne valve flowbodies were cast from the first titaniumaluminide alloy (identified as “Example 1” in the table below) andweighed approximately 1,791.83 grams and 1,797.36 grams. By comparison,a nominally identical valve flowbody cast from an Inconel 718® alloyweighed approximately 3,383.14 grams, approximately 89% heavier than thevalve flowbodies cast from the first titanium aluminide alloy (“Example1”). In other words, the TiAl valve flowbodies weighed approximately 47%less than the nominally identical Inconel 718® valve flowbody. Fewerstructural defects were detected within the valve flowbodies cast fromthe first titanium aluminide alloy (“Example 1”) than within the valveflowbody cast from the second titanium aluminide alloy (“Example 2”).

Example 1 Example 2 Component At. % At. % Titanium 50.2 51.4 Aluminum45.0 43.5 Manganese 2.0 — Niobium 2.0 4.0 Boron — 0.1 Molybdenum — 1.0Titanium Diboride 0.8 —

Exemplary valve flowbodies cast from the first TiAl alloy (identified as“Example 1” above) were further machined by mechanical means to createflanges with desired dimensions and properties. A flowbody with themachined flange was connected to a mating flange of a test system, usinga V-band clamp, and clamped successfully in place, using standardprocedures. No damage to the flange of the TiAl flowbody was visibleafter this clamping test, and this flange further successfully passed apost-clamping test fluorescent penetrant inspection (FPI) procedure.

In view of the above, it should be appreciated that there has beenprovided multiple exemplary embodiments of a lightweight, hightemperature airborne valve including a flowbody formed, at leastpartially, from a titanium aluminide alloy. The foregoing has alsoprovided at least one exemplary embodiment of a method for manufacturingsuch a lightweight, high temperature airborne valve. While, in theabove-described embodiments, the airborne valve assumed the form of acylindrically-shaped butterfly valve, alternative embodiments of thepresent invention may assume various other forms, including those of aright-angle poppet valve and an inline poppet valve. In certainembodiments, other machined or hot isostatic pressed parts can be bondedor otherwise joined to the titanium aluminide flowbody utilizing, forexample, brazing or welding.

While at least one exemplary embodiment has been presented in theforegoing Detailed Description, it should be appreciated that a vastnumber of variations exist. It should also be appreciated that theexemplary embodiment or exemplary embodiments are only examples, and arenot intended to limit the scope, applicability, or configuration of theinvention in any way. Rather, the foregoing Detailed Description willprovide those skilled in the art with a convenient road map forimplementing an exemplary embodiment of the invention. It beingunderstood that various changes may be made in the function andarrangement of elements described in an exemplary embodiment withoutdeparting from the scope of the invention as set-forth in the appendedClaims.

What is claimed is:
 1. A method for producing a lightweight, hightemperature airborne valve, the method comprising the steps of:selecting a near-stoichiometric titanium aluminide alloy having adensity between approximately 3.5 grams per cubic centimeter andapproximately 5.0 grams per cubic centimeter; pouring the selectednear-stoichiometric titanium aluminide alloy into a mold in an enclosuresubstantially devoid of oxidants to form a lightweight flowbody having aflow passage extending therethrough; removing the lightweight flowbodyfrom the mold; hot isostatic pressing the lightweight flowbody;machining the lightweight flowbody to desired dimensions; and mounting avalve element in the flow passage of the lightweight flowbody.
 2. Themethod of claim 1 wherein the lightweight flowbody is fabricated toinclude a radial mounting flange, and wherein the method furthercomprises installing the lightweight, high temperature airborne valvewithin a pneumatic avionic system deployed aboard an aircraft andutilized to regulate the flow of pressurized air or combustive gassesbled from a gas turbine engine during operation thereof.
 3. The methodof claim 1 further comprising applying an oxidation-resistant coatingover at least one surface of the lightweight flowbody after machiningthe lightweight flowbody to desired dimensions.
 4. The method of claim 3wherein applying comprises applying an oxidation-resistant coating overthe interior surfaces of the flow passage exposed to hot gas flow duringoperation of the lightweight, high temperature airborne valve.
 5. Themethod of claim 1 wherein the valve element comprises: a butterfly discrotatably mounted within the flow passage; and a wiper seal carried bythe butterfly disc and sealingly engaging an inner surface of thelightweight flowbody; and wherein the method further comprises applyinga wear-resistant coating over the inner surface of the flow passagecontacted by the wiper seal during rotation of the butterfly disc. 6.The method of claim 1 further comprises bonding at least one machined orhot isostatic pressured part to the titanium aluminide flowbody aftermachining.
 7. The method of claim 1 wherein selecting comprisesselecting a near-stoichiometric titanium aluminide including at leastone of the group consisting of manganese, boron, niobium, molybdenum,and titanium diboride and added to a master alloy during processing ofthe titanium aluminide alloy.
 8. The method of claim 1 wherein theselecting comprises selecting a near-stoichiometric titanium aluminidealloy comprising titanium, aluminum, manganese, niobium, and titaniumdiboride.
 9. The method of claim 8 wherein selecting comprises selectinga near-stoichiometric titanium aluminide alloy comprising, by weight:about 50.2% titanium; about 45.0% aluminum; about 2.0% manganese; about2.0% niobium; and about 0.8% titanium diboride.
 10. The method of claim1 wherein selecting comprises selecting a near-stoichiometric titaniumaluminide alloy comprising titanium, aluminum, niobium, boron, andmolybdenum.
 11. The method of claim 10 wherein selecting comprisesselecting a near-stoichiometric titanium aluminide alloy comprising, byweight: about 51.4% titanium; about 43.5% aluminum; about 4.0% niobium;about 0.1% boron; and about 1.0% molybdenum.
 12. A method, comprising:obtaining a high temperature airborne valve, comprising: a lightweightflowbody formed substantially entirely of a near-stoichiometric titaniumaluminide alloy having a density between approximately 3.5 grams percubic centimeter and approximately 5.0 grams per cubic centimeter; and aradial mounting flange extending from the lightweight flowbody; andinstalling the high temperature airborne valve in a pneumatic avionicsystem deployed onboard an aircraft by clamping the radial mountingflange of the high temperature airborne valve to a duct included in thepneumatic avionic system and conducting pressurized air flow orcombustive gas flow bled from a gas turbine engine during operationthereof.
 13. The method of claim 12 wherein obtaining comprisesobtaining a high temperature airborne valve having a lightweightflowbody formed substantially entirely of a near-stoichiometric titaniumalloy comprising titanium, aluminum, manganese, niobium, and titaniumdiboride.
 14. The method of claim 12 wherein obtaining comprisesobtaining a high temperature airborne valve having a lightweightflowbody formed substantially entirely of a near-stoichiometric titaniumalloy comprising titanium, aluminum, niobium, boron, and molybdenum. 15.A method for producing a lightweight, high temperature airborne valve,the method comprising the steps of: selecting a titanium aluminide alloycontaining at least one of the group consisting of manganese, boron,niobium, molybdenum, and titanium diboride and added to a master alloyduring processing of the titanium aluminide alloy; pouring the selectedtitanium aluminide alloy into a mold in an enclosure substantiallydevoid of oxidants to form a lightweight flowbody having a flow passageextending therethrough; removing the lightweight flowbody from the mold;machining the lightweight flowbody to desired dimensions; and mounting avalve element in the flow passage of the lightweight flowbody.
 16. Themethod of claim 15 wherein the selecting comprises selecting a titaniumaluminide alloy comprising titanium, aluminum, manganese, niobium, andtitanium diboride.
 17. The method of claim 16 wherein selectingcomprises selecting a titanium aluminide alloy comprising, by weight:about 50.2% titanium; about 45.0% aluminum; about 2.0% manganese; about2.0% niobium; and about 0.8% titanium diboride.
 18. The method of claim15 wherein selecting comprises selecting a titanium aluminide alloycomprising titanium, aluminum, niobium, boron, and molybdenum.
 19. Themethod of claim 18 wherein selecting comprises selecting a titaniumaluminide alloy comprising, by weight: about 51.4% titanium; about 43.5%aluminum; about 4.0% niobium; about 0.1% boron; and about 1.0%molybdenum.
 20. The method of claim 15 wherein selecting comprisesselecting a titanium aluminide alloy formulated to have atitanium-to-aluminide ratio of approximately 1:1 on the atomic scale.